747-400 AMM 飞机维护手册 发动机 ENGINE 1(159)

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ENGINES PRE-PHASE III L-A8821 (0896)
1st-Stage Fan Blade Damage Limits Figure 602 (Sheet 1)
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1st-Stage Fan Blade Damage Limits
Figure 602 (Sheet 2)

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Names of the Fan Blade Shroud Areas
Figure 603

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B-B 
ENGINES PRE-PHASE III 
ENGINES POST-PHASE III 
Fan Blade Shroud Damage Limits 
Figure 604 

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LEADING EDGE

SEE

A-A

1
DIMEMSIONS APPLY TO ENGINES PRE- AND POST-PHASE III L-A1066
1st-Stage Blade Platform Inspection Limits Figure 606
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1st-Stage Blade Leading and Trailing Edge Root Blend Limits
Figure 607

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SEE  A 
AREA A  1 
　
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